gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
|
gptkb:aircraft
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gptkbp:compression_ratio
|
6.5:1
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gptkbp:configuration
|
14-cylinder
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gptkbp:cooling_system
|
air-cooled
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gptkbp:country_of_origin
|
gptkb:United_Kingdom
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gptkbp:displacement
|
2,000 cubic inches
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gptkbp:engine
|
gptkb:Bristol_Aeroplane_Company
advanced for its time
supercharged
limited production run
used in several aircraft models
introduced new engineering techniques
remains a notable example of British engineering.
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gptkbp:engine_configuration
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gptkb:Bristol_Aeroplane_Company
radial
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gptkbp:engine_power
|
high reliability
good performance at altitude
1,500 hp at 2,700 rpm
|
gptkbp:engine_type
|
piston engine
compatible with various aircraft designs
Proteus 600, Proteus 700
|
gptkbp:fuel_capacity
|
3 ft 6 in
4 ft 6 in
|
gptkbp:fuel_economy
|
moderate fuel efficiency
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gptkbp:fuel_type
|
aviation gasoline
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Proteus
|
gptkbp:impact
|
influenced future engine designs
|
gptkbp:maintenance
|
moderate maintenance requirements
|
gptkbp:manufacturer
|
gptkb:Bristol_Aeroplane_Company
|
gptkbp:noise_level
|
low vibration levels
notable noise levels
|
gptkbp:notable_feature
|
double-row design
|
gptkbp:number_of_engines
|
gptkb:14
|
gptkbp:original_run
|
1945
|
gptkbp:power_output
|
1,500 hp
|
gptkbp:production_years
|
1945-1955
|
gptkbp:propeller
|
variable-pitch propeller
|
gptkbp:successor
|
gptkb:Bristol_Centaurus
|
gptkbp:torque
|
1,200 lb-ft
|
gptkbp:type
|
gptkb:radial_engine
|
gptkbp:used_in
|
gptkb:Bristol_Brabazon
|
gptkbp:weight
|
1,200 lb
|
gptkbp:bfsParent
|
gptkb:Vickers_Vanguard
|
gptkbp:bfsLayer
|
5
|